HIGH SPEED YAW CONTROL SYSTEM FOR ROTARY WING AIRCRAFT - Patent 0600990

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EP 0 600 990 A1

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(43)	Date of publication:
	15.06.1994 Bulletin 1994/24

(21)	Application number: 92917932.0

(22)	Date of filing: 31.07.1992

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International Patent Classification (IPC):

B64C 13/ 50^{( . )}
G05D 1/ 08^{( . )}

G05D 1/ 00^{( . )}

(86)	International application number:
	PCT/US1992/006427

(87)	International publication number:
	WO 1993/005458 (18.03.1993 Gazette 1993/08)

(84)	Designated Contracting States:
	DE FR GB IT

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Priority:

28.08.1991 US 19910751432

(71)	Applicant: UNITED TECHNOLOGIES ELECTRO SYSTEMS, INC.
	Hartford Connecticut 06101 (US)

(72)	Inventors:
	WRIGHT, Stuart, C. Woodbridge, CT 06525 (US) ADAMS, Don, L. Fairfield, CT 06430 (US) GOLD, Phillip, J. Shelton, CT 06484 (US)

(74)	Representative: Klunker . Schmitt-Nilson . Hirsch
	Winzererstrasse 106 D-80797 München D-80797 München (DE)

(54)	HIGH SPEED YAW CONTROL SYSTEM FOR ROTARY WING AIRCRAFT